gruntguru wrote: ↑13 Nov 2025, 04:57
I get your point. It is really only the ICE that converts fuel energy to mechanical - and that includes the turbo-compounding. Current efficiency of 50%+ includes a very minor loss converting turbine energy to electrical.
Does anyone have any thoughts on how the ICE might change and what efficiency might be possible, now that the only source of work is the crankshaft?
My initial thoughts:
1. Later EVO to increase in-cylinder expansion and minimise EGT.
2. Reduce or eliminate EIVC (Miller) to maximise pumping work done on piston during intake stroke. (This will be the sole means of returning recovered exhaust energy to the PU)
3. Larger turbine and housing to reduce backpressure. Minimise wastegating.
3. The size of the turbo is restrcited by the rules.
C5.3.5 Referring to Drawing 4 of Appendix C3, the turbocharger compressor and turbine must satisfy the following dimensional constraints. Only compressor and turbine wheels approved by the FIA Technical Department will be allowed:
a. The
compressor exducer blade outer diameter (A) must lie
between 100mm and 110mm. For the avoidance of doubt, no part of the compressor wheel (including blades, hub and any blade/hub fillet radius) can have a diameter more than the upper limit and the maximum diameter of the compressor wheel (including blades, hub and any blade/hub fillet radius) cannot have a diameter smaller than the lower limit.
b. The
compressor axial distance from the outside diameter of the inducer blade edge to rear plane of exducer, at its outer diameter (B) must lie
between 30mm and 35mm
c. The
turbine inducer blade outer diameter (C) must lie
between 90mm and 100mm. For the avoidance of doubt, no part of the turbine wheel (including blades, hub and any blade/hub fillet radius) can have a diameter more than the upper limit and the maximum diameter of the turbine wheel (including blades, hub and any blade/hub fillet radius) cannot have a diameter smaller than the lower limit.
d. The
turbine axial distance from the outside diameter of the exducer blade edge to forward plane of inducer, at its outer diameter (D) must lie
between 35mm and 40mm
e. The maximum distance between the rear of the compressor exducer and the front of the turbine inducer (E) will be 175mm
Not sure how that relates to minimising back pressure.